The law enforcement standoff inspection drone capability (L-SID) integrates Various technology to enable a capability implemented at the squad car level to allow the first-to-scene the ability to remotely pre-screen the scene for threat, before an on-foot approach. This is accomplished with an officer launched and controlled and specially configure small unmanned aircraft system (UAS). The LAS is integrated with a specially configured one-hand drone controller, a wearable see through heads-up-display glasses, microphone that's linked to the UAS's onboard loudspeaker, and a special processing that enables looking through a vehicle of building tinted windows during enforcement event. The system operates on a private ad-hoc network, implements IEEE 802.1 1 g/n WPA 3 standards, and provides continuous live steamed scene data throughout the enforcement event. All data and video collected is transmitted in real-time to headquarters.

An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from an access management device and other devices connected to the software platform. Other devices connected to the platform include robots, such as aerial robots, which are configured to detect motion and engage with an object connected to the motion detection. An enclosure is operable to house an aerial robot and provides for ease of addition of the aerial robot to a security or entry management system by providing an easily installable package. The enclosure provides the advantages of simple deployment and charging of aerial robots.

An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from an access management device and other devices connected to the software platform. Other devices connected to the platform include robots, such as aerial robots, which are configured to detect motion and engage with an object connected to the motion detection. An enclosure is operable to house an aerial robot and provides for ease of addition of the aerial robot to a security or entry management system by providing an easily installable package. The enclosure provides the advantages of simple deployment and charging of aerial robots.

A connection apparatus of a detachable gimbal and an unmanned aerial vehicle are disclosed. The connection apparatus of a detachable gimbal includes: an alignment component, where the alignment component is configured to align a circuit connection terminal of an unmanned aerial vehicle with a circuit connection terminal of a gimbal; a pre-installed component disposed on the alignment component, where the pre-installed component moves relative to the alignment component to fixedly connect the gimbal to a fuselage of the unmanned aerial vehicle; and a locking component disposed on the pre-installed component, where the locking component locks the pre-installed component when the pre-installed component moves relative to the alignment component to a preset location.

A spectral camera control device, being installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight. The spectral camera control device causes the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of the liquid crystal tunable filter is switched while the aircraft is in stationary flight, and the spectral camera control device causes a plurality of spectral images to be captured in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

A spectral camera control device, being installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight. The spectral camera control device causes the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of the liquid crystal tunable filter is switched while the aircraft is in stationary flight, and the spectral camera control device causes a plurality of spectral images to be captured in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

Provided are an action plan making system and method for an unmanned aerial vehicle, and a storage medium. The action plan making system (1) includes: an unmanned aerial vehicle (10), provided with an aerial shooting device; and a computer (30). A control unit of the computer (30) executes a making module (324), which makes an action plan including a flight plan and a shooting plan of the unmanned aerial vehicle (10) according to a region accepted by executing a region acceptance module (322) and a purpose accepted by executing a purpose acceptance module (323). A control unit (14) of the unmanned aerial vehicle (10) executes a control module (141), and controls the aerial shooting of a camera (17) and flying of the unmanned aerial vehicle (10) based on the action plan made by executing the making module (324) by the control unit (32) of the computer (30).

Provided are an action plan making system and method for an unmanned aerial vehicle, and a storage medium. The action plan making system (1) includes: an unmanned aerial vehicle (10), provided with an aerial shooting device; and a computer (30). A control unit of the computer (30) executes a making module (324), which makes an action plan including a flight plan and a shooting plan of the unmanned aerial vehicle (10) according to a region accepted by executing a region acceptance module (322) and a purpose accepted by executing a purpose acceptance module (323). A control unit (14) of the unmanned aerial vehicle (10) executes a control module (141), and controls the aerial shooting of a camera (17) and flying of the unmanned aerial vehicle (10) based on the action plan made by executing the making module (324) by the control unit (32) of the computer (30).

Techniques involve releasing and/or capturing a fixed-wing aircraft using an aerial vehicle with VTOL capabilities while the fixed-wing aircraft is in flight. For example, the VTOL aerial vehicle may take off vertically while carrying the fixed-wing aircraft and then fly horizontally before releasing the fixed-wing aircraft. Upon release, the fixed-wing aircraft flies independently to perform a mission (e.g., surveillance, payload delivery, combinations thereof, etc.). After the fixed-wing aircraft has completed its mission, the VTOL aerial vehicle may capture the fixed-wing aircraft while both are in flight, and then land together vertically. Such operation enables the fixed-wing aircraft to vertically take off and/or land while avoiding certain drawbacks associated with a conventional VTOL kit such as being burdened by weight and drag from the VTOL kit's rotors/propellers, mounting hardware, etc. during a mission which otherwise would limit the fixed-wing aircraft's maximum airspeed, ceiling, payload capacity, endurance, and so on.

Techniques involve releasing and/or capturing a fixed-wing aircraft using an aerial vehicle with VTOL capabilities while the fixed-wing aircraft is in flight. For example, the VTOL aerial vehicle may take off vertically while carrying the fixed-wing aircraft and then fly horizontally before releasing the fixed-wing aircraft. Upon release, the fixed-wing aircraft flies independently to perform a mission (e.g., surveillance, payload delivery, combinations thereof, etc.). After the fixed-wing aircraft has completed its mission, the VTOL aerial vehicle may capture the fixed-wing aircraft while both are in flight, and then land together vertically. Such operation enables the fixed-wing aircraft to vertically take off and/or land while avoiding certain drawbacks associated with a conventional VTOL kit such as being burdened by weight and drag from the VTOL kit's rotors/propellers, mounting hardware, etc. during a mission which otherwise would limit the fixed-wing aircraft's maximum airspeed, ceiling, payload capacity, endurance, and so on.